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Printed page xii. PDF page 14.
flight crew and cabin crew managed the event as a competent team in accordance with standard operating procedures and practices. Damage to the aircraft The aircraft sustained damage from a large number of disc fragments and associated debris. The damageOpen official document at PDF page 14ATSB AO-2010-089: In-flight uncontained engine failure, Airbus A380-842 VH-OQA, overhead Batam Island, 4 November 2010
Printed page 6. PDF page 26.
a foam blanket over the fuel leak in accordance with the airport emergency services standard operating procedures. The flight crew then discussed the options for disembarking the passengers. The captain made a PA announcement to the cabin crew and passengersOpen official document at PDF page 26ATSB AO-2010-089: In-flight uncontained engine failure, Airbus A380-842 VH-OQA, overhead Batam Island, 4 November 2010
Printed page 131. PDF page 151.
continued safe flight and landing. Furthermore, the flight crew operated in accordance with standard operating procedures and practices. Therefore, this analysis is focused on the failure of the No. 2 engine and the factors that lead to the failure. ThisOpen official document at PDF page 151ATSB AO-2010-089: In-flight uncontained engine failure, Airbus A380-842 VH-OQA, overhead Batam Island, 4 November 2010
Printed page 146. PDF page 166.
The flight and cabin crew managed the event as a competent team in accordance with standard operating procedures and practices. - 146 -Open official document at PDF page 166ATSB AO-2010-089: In-flight uncontained engine failure, Airbus A380-842 VH-OQA, overhead Batam Island, 4 November 2010